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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine gives ________ efficiency as compared to an open cycle gas turbine.

Same
None of these
Lower
Higher

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Compressors, Gas Turbines and Jet Engines
In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as

Pressure coefficient
Work factor
Slip factor
Degree of reaction

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Compressors, Gas Turbines and Jet Engines
In multistage compressor, the isothermal compression is achieved by

By running compressor at very slow speed
By insulating the cylinder
By constantly cooling the cylinder
Employing inter-cooler

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Compressors, Gas Turbines and Jet Engines
The efficiency of the vane blower is (where W₁ = Workdone due to compression, and W₂ = Workdone due to back flow)

(W₁ + W₂)/W₁
(W₁ + W₂)/W₂
W₂/(W₁ + W₂)
W₁/(W₁ + W₂)

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In three phases
In a single phase
In two phases
In the form of air and water mixture

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Compressors, Gas Turbines and Jet Engines
Reheating in a multistage expansion gas turbine ________ compressor work.

None of these
Decreases
Has no effect on
Increases

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